WORTMANN FX 80-080 (fx80080-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: WORTMANN FX 80-080 (fx80080-il) Reynolds number: 1,000,000 Max Cl/Cd: 123.6 at α=2.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx80080-il-1000000.txt Download as CSV file: xf-fx80080-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 80-080
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.3472 0.08284 0.08132 -0.0343 1.0000 0.0082
-9.250 -0.3496 0.07846 0.07696 -0.0351 1.0000 0.0083
-9.000 -0.3513 0.07447 0.07299 -0.0358 1.0000 0.0083
-8.750 -0.3550 0.07014 0.06867 -0.0366 1.0000 0.0083
-6.250 -0.3236 0.02048 0.01697 -0.0847 0.9508 0.0085
-6.000 -0.2880 0.01849 0.01467 -0.0872 0.9432 0.0084
-5.750 -0.2554 0.01416 0.00971 -0.0895 0.9351 0.0087
-5.500 -0.2242 0.01203 0.00727 -0.0908 0.9263 0.0092
-5.250 -0.1945 0.01099 0.00608 -0.0914 0.9177 0.0098
-5.000 -0.1645 0.01046 0.00545 -0.0921 0.9101 0.0108
-4.750 -0.1382 0.00985 0.00474 -0.0919 0.9023 0.0116
-4.250 -0.0849 0.00898 0.00367 -0.0915 0.8893 0.0129
-4.000 -0.0586 0.00851 0.00310 -0.0913 0.8835 0.0138
-3.750 -0.0339 0.00789 0.00237 -0.0907 0.8779 0.0168
-3.500 -0.0074 0.00768 0.00211 -0.0905 0.8726 0.0195
-3.250 0.0199 0.00744 0.00177 -0.0904 0.8680 0.0241
-3.000 0.0456 0.00718 0.00157 -0.0900 0.8631 0.0399
-2.750 0.0720 0.00698 0.00143 -0.0898 0.8585 0.0634
-2.500 0.0990 0.00678 0.00132 -0.0898 0.8543 0.1019
-2.250 0.1241 0.00644 0.00122 -0.0895 0.8500 0.1775
-2.000 0.1473 0.00578 0.00110 -0.0890 0.8455 0.3560
-1.750 0.1691 0.00500 0.00102 -0.0883 0.8414 0.5936
-1.500 0.1935 0.00477 0.00106 -0.0876 0.8374 0.6980
-1.250 0.2201 0.00473 0.00107 -0.0872 0.8332 0.7281
-1.000 0.2470 0.00473 0.00107 -0.0870 0.8290 0.7481
-0.750 0.2740 0.00475 0.00110 -0.0867 0.8245 0.7688
-0.500 0.3003 0.00474 0.00111 -0.0863 0.8188 0.7815
-0.250 0.3272 0.00477 0.00112 -0.0860 0.8131 0.7949
0.000 0.3531 0.00477 0.00115 -0.0855 0.8069 0.8083
0.250 0.3793 0.00479 0.00117 -0.0851 0.8005 0.8201
0.500 0.4053 0.00480 0.00119 -0.0846 0.7932 0.8306
0.750 0.4314 0.00484 0.00120 -0.0841 0.7850 0.8396
1.000 0.4572 0.00481 0.00121 -0.0836 0.7759 0.8461
1.250 0.4834 0.00483 0.00122 -0.0831 0.7657 0.8516
1.500 0.5096 0.00485 0.00122 -0.0828 0.7559 0.8565
1.750 0.5353 0.00486 0.00123 -0.0822 0.7433 0.8614
2.000 0.5614 0.00490 0.00126 -0.0818 0.7306 0.8665
2.250 0.5865 0.00494 0.00130 -0.0812 0.7104 0.8713
2.500 0.6111 0.00502 0.00134 -0.0804 0.6874 0.8767
2.750 0.6353 0.00514 0.00139 -0.0796 0.6577 0.8826
3.000 0.6561 0.00539 0.00148 -0.0781 0.6011 0.8892
3.250 0.6726 0.00598 0.00169 -0.0758 0.5021 0.8976
3.500 0.6863 0.00682 0.00203 -0.0732 0.3724 0.9077
3.750 0.7015 0.00760 0.00235 -0.0709 0.2566 0.9202
4.000 0.7202 0.00815 0.00263 -0.0693 0.1797 0.9380
4.250 0.7493 0.00864 0.00292 -0.0700 0.1236 0.9670
4.500 0.7786 0.00908 0.00321 -0.0707 0.0871 1.0000
4.750 0.8024 0.00945 0.00349 -0.0701 0.0653 1.0000
5.000 0.8265 0.00979 0.00377 -0.0696 0.0500 1.0000
5.250 0.8501 0.01017 0.00407 -0.0689 0.0362 1.0000
5.500 0.8735 0.01056 0.00441 -0.0682 0.0258 1.0000
5.750 0.8965 0.01100 0.00486 -0.0673 0.0199 1.0000
6.000 0.9206 0.01132 0.00519 -0.0668 0.0170 1.0000
6.250 0.9416 0.01197 0.00590 -0.0655 0.0133 1.0000
6.500 0.9660 0.01224 0.00619 -0.0650 0.0122 1.0000
6.750 0.9896 0.01259 0.00654 -0.0644 0.0101 1.0000
7.000 1.0065 0.01372 0.00780 -0.0623 0.0079 1.0000
7.250 1.0300 0.01407 0.00819 -0.0617 0.0073 1.0000
7.500 1.0525 0.01455 0.00870 -0.0608 0.0062 1.0000
7.750 1.0740 0.01513 0.00935 -0.0598 0.0056 1.0000
8.000 1.0904 0.01635 0.01068 -0.0579 0.0049 1.0000
8.250 1.1061 0.01780 0.01230 -0.0559 0.0046 1.0000
8.500 1.1250 0.01882 0.01345 -0.0545 0.0045 1.0000
8.750 1.1441 0.01984 0.01460 -0.0532 0.0044 1.0000
9.000 1.1623 0.02098 0.01589 -0.0517 0.0042 1.0000
9.250 1.1794 0.02228 0.01735 -0.0502 0.0041 1.0000
9.500 1.1948 0.02386 0.01912 -0.0484 0.0040 1.0000
9.750 1.2095 0.02533 0.02078 -0.0466 0.0038 1.0000
10.000 1.2266 0.02601 0.02157 -0.0452 0.0035 1.0000
10.250 1.2319 0.02879 0.02467 -0.0421 0.0035 1.0000
10.500 1.2399 0.03050 0.02658 -0.0395 0.0034 1.0000
10.750 1.2532 0.03064 0.02674 -0.0375 0.0031 1.0000
11.000 1.2545 0.03234 0.02861 -0.0340 0.0031 1.0000
11.250 1.2511 0.03445 0.03095 -0.0301 0.0030 1.0000
11.500 1.2453 0.03634 0.03296 -0.0264 0.0028 1.0000
11.750 1.2347 0.03909 0.03595 -0.0228 0.0028 1.0000
12.000 1.2225 0.04210 0.03918 -0.0198 0.0028 1.0000
12.250 1.1941 0.04698 0.04435 -0.0168 0.0027 1.0000
12.500 1.1781 0.05092 0.04848 -0.0155 0.0027 1.0000
12.750 1.1671 0.05465 0.05237 -0.0151 0.0028 1.0000
13.000 1.1428 0.06053 0.05845 -0.0160 0.0028 1.0000
13.250 1.1128 0.06856 0.06672 -0.0190 0.0029 1.0000
13.500 1.0990 0.07480 0.07304 -0.0229 0.0028 1.0000
13.750 1.0741 0.08578 0.08418 -0.0306 0.0028 1.0000
|
Polar data table (+)
Polar graphs
<< Back to WORTMANN FX 80-080 (fx80080-il)